View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20804U 90083A 23342.52150973 .00000063 00000-0 51090-4 0 9998
2 20804 82.9379 130.3253 0036121 328.7172 98.9454 13.74425185666629
Epoch (UTC): | 08 December 2023 12:30:58 |
Eccentricity: | 0.0036121 |
inclination: | 82.9379° |
perigee height: | 957 km |
apogee height: | 1010 km |
right ascension of ascending node: | 130.3253° |
argument of perigee: | 328.7172° |
revolutions per day: | 13.74425185 |
mean anomaly at epoch: | 98.9454° |
orbit number at epoch: | 66662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|